View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 56318U 26145.46486086 +.00000000 +00000-0 +59919-4 0 00003
2 56318 97.4474 146.5899 0002115 101.4774 258.6691 15.05658009 01
| Epoch (UTC): | 25 May 2026 11:09:23 |
| Eccentricity: | 0.0002115 |
| inclination: | 97.4474° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 146.5899° |
| argument of perigee: | 101.4774° |
| revolutions per day: | 15.05658009 |
| mean anomaly at epoch: | 258.6691° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|